N380NG
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
20 reports on file, 2011-11-29 – 2014-12-30.
Part: SKIN — NICKED (BS 94) · airframe 5,507 hrs · 5,303 cycles
DURING HEAVY CHECK, FOUND SMALL NICK TO ACFT SKIN AT BS 94.800, STR 29R. MX PERFORMED PERMANENT REPAIR IAW RD8/4-53-6617, SKIN, PN 85327051, REF EMERY PO 4591 FOR MATERIAL USED .063, 2024-T3 P/SHEET.
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 5,507 hrs · 5,303 cycles
DURING HEAVY CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK. MAINTENANCE R & R THE SEAT TRACK IAW SRM 51-40-15, 51-41-00, 51-42-05.
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 5,507 hrs · 5,303 cycles
DURING HEAVY CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK. R & R THE SEAT TRACK IAW SRM 51-40-07, 51-40-10, AND 51-42-05.
Part: SKIN — DENTED (ZONE 200) · airframe 5,507 hrs · 5,303 cycles
DENTS ON RT FUSELAGE BETWEEN BS 281 - 301 AND STR 16 - 20S. AFT OF ICE SHIELD BELOW WINDOW. MAINTENANCE PERFORMED MAJOR REPAIR IAW RD 8/4-53-6589, ISSUE 1. & SRM 51-42-05 AND 51-40-07.
Part: SKIN — DENTED (ZONE 200) · airframe 5,507 hrs · 5,303 cycles
DURING HEAVY CHECK, FUSELAGE SKIN DENTED BY BIRD STRIKES. REPAIRED IAW SRM 51-25-05-02-01, 51-42-05-02-01.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 5,507 hrs · 5,303 cycles
MAINTENANCE FOUND CORROSION ON THE ACCESS PANEL LANDING. MAINTENANCE REPAIRED AREA IAW RD 8/4-57-2694.
Part: FLASHLIGHT — MISSING (FWD CABIN) · airframe 5,310 hrs · 5,120 cycles
CREW REPORTED THAT THE FORWARD F/A FLASHLIGHT WAS MISSING. MAINTENANCE INSTALLED A NEW FLASHLIGHT IAW AMM.
Part: GUIDE STOP — FAILED (PAX DOOR) · airframe 4,846 hrs · 4,680 cycles
CREW REPORTED THAT THE MAIN CABIN DOOR WOULD NOT OPEN. MAINTENANCE TROUBLESHOT AND FOUND A BAD GUIDE STOP AND CAP. MAINTENANCE R & R GUIDE STOP AND CAP IAW AMM AND OPS CHECKED GOOD.
Part: BATTERY — INOPERATIVE (MEGAPHONE) · airframe 4,786 hrs · 4,620 cycles
CREW REPORTED THAT THE MEGAPHONE BATTERY WAS INOPERATIVE. MAINTENANCE R & R THE BATTERY IAW AMM AND OPS CHECKED GOOD.
Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 4,399 hrs · 4,256 cycles
CREW REPORTED THAT BOTH COCKPIT FLASHLIGHTS WERE INOPERATIVE. MAINTENANCE R & R THE FLASHLIGHTS BATTERIES IAW AMM AND OPS CHECKED GOOD.
Part: FLASHLIGHT — MISSING (COCKPIT) · airframe 4,362 hrs · 4,219 cycles
CREW REPORTED THAT BOTH COCKPIT FLASHLIGHTS WERE MISSING.
Earlier reports · 2011–2013 · 9 reports
2013
Part: FLASHLIGHT — INOPERATIVE (ZONE 900) · airframe 3,659 hrs · 3,553 cycles
AFT F/A FLASHLIGHT WAS FOUND TO BE INOPERATIVE. SECURED FLASHLIGHT ENDCAP IAW AMM 25-00-00. OPS CHECKED GOOD.
Part: WARNING LIGHT — FALSE ACTIVATION (CARGO DOOR) · airframe 3,563 hrs · 3,463 cycles
CREW LEVELED OFF AT 11,000 FEET AND RECEIVED "FUSELAGE DOORS" WARNING LIGHT. AFT CARGO DOOR INDICATED RED AND CREW RAN QRH. F/A CALLED COCKPIT AND ADVISED SHE HEARD "BANGING" NOISES FROM THE CARGO BIN AND THAT IT WAS COLD IN THE REAR OF THE PLANE. CREW DECLARED AN EMERGENCY AND RETURNED, LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND BAGGAGE LEANING HARD AGAINST THE CARGO NET. MAINTENANCE PERFORMED OPS CHECK OF THE AFT BAGGAGE DOOR AMM AND NO FAULTS WERE FOUND. AIRCRAFT IS GOOD FOR SERVICE.
Part: BLOWOUT PANEL — POPPED · airframe 3,509 hrs · 3,412 cycles
CREW STATED THAT THE FUSELAGE DOORS WARNING LIGHT CAME ON DURING ROTATION AND THE ACFT DUMPED PRESSURE. AN EMERGENCY WAS NOT DECLARED AND RETURNED TO LAND WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND AFT BLOW OUT PANEL WAS POPPED. MAINTENANCE SECURRED AFT BLOW OUT PANEL AND PERFORMED A GROUND PRESSURE CHECK IAW AMM. ACFT IS GOOD FOR SERVICE.
Part: HANDLE — UNSECURE (AFT CARGO DOOR) · airframe 3,504 hrs · 3,406 cycles
CREW RECEIVED FUSELAGE DOOR WARNING LIGHT THAT INDICATED THE AFT CARGO BAY DOOR WAS OPEN. AN EMERGENCY WAS NOT DECLARED, ACFT LOST PRESSURIZATION AT 6000 FT. LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED IAW AMM AND FOUND THE AFT BAGGAGE DOOR HANDLE POPPED OPEN. NO DISCREPANCIES WERE NOTED AND BLOW OUT PLANELS IN AFT CARGO BAY WERE INTACT. ACFT IS GOOD FOR SERVICE.
Part: PSU — DISLODGED (CABIN) · airframe 3,151 hrs · 3,059 cycles
CREW REPORTED THAT THE PSU PANEL FELL DOWN AFTER LANDING. MX SECURED PANEL IAW AMM AND OPS CHECKED GOOD. ACFT IS GOOD FOR SERVICE.
Part: TRIM SYSTEM — MALFUNCTIONED (ZONE 600) · airframe 2,911 hrs · 2,816 cycles
DURING CRUISE, RECEIVED A PITCH TRIM CAUTION LIGHT. AUTOPILOT WAS DISENGAGED AND TRIED TO ACTIVATE THE PITCH TRIM WITH NO SUCCESS. AS ACFT SLOWED DOWN, FORCE NEEDED TO MOVE THE ELEVATORS INCREASED. DECLARED AN EMERGENCY. FLAPS WERE EXTENDED TO 35 AS IT PROVIDED THE MOST CONTROL AND LANDED WITHOUT INCIDENT. OPS CHECKED PITCH TRIM SYS PER AMM AND NO FAULTS FOUND. AS A PRECAUATION, RT ELEVATOR PITCH TRIM ACTUATOR WAS REPLACED THE NEXT NIGHT IAW AMM AND ACFT IS GOOD FOR SERVICE. P
Part: HANDLE — OUT OF ADJUST (AFT CARGO DOOR) · airframe 2,702 hrs · 2,618 cycles
CREW RECEIVED AN AFT BAGGAGE WARNING LIGHT DURING CLIMB OUT. ACFT PRESSURIZED NORMALLY AND CREW CONTINUED. F/A`S HEARD SOUND OF AFT BAGGAGE DOOR SLAMMING SHUT AROUND 4000 FT ON DESCENT. AN EMERGENCY WAS NOT DECLARED AND ACFT LANDED WITHOUT INCIDENT. MX FOUND THE SILVER BAGGAGE HANDLE WAS POPPED OUT AT THE GATE. MX PERFORMED ADJUSTMENT TEST OF AFT BAGGAGE DOOR IAW AMM AND OPS CHECKED GOOD.
Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 2,184 hrs · 2,108 cycles
WHILE EN ROUTE FROM DEN TO MCI CREW REPORTED THE AFT BAGGAGE DOOR FUSELAGE WARNING LIGHT CAME ON AND THE DOOR SHOWED OPEN ON THE MFD, HOWEVER PRESSURIZATION WAS NORMAL. CREW DID NOT DECLARE AND EMERGENCY AND ELECTED TO RETURN TO DEN WHERE THEY LANDED WITHOUT INCIDENT. DOOR WAS OPEN AND CLOSED BY THE RAMP BEFORE MAINTENANCE COULD CONFIRM POSITION OF THE HANDLE. MAINTENANCE PERFORMED OPS CHECK OF THE DOOR PER BOMBA AMM AND OPS CHECKED GOOD.
2011
Part: ENGINE — POWER LOSS (NR 2) · airframe 566 hrs · 532 cycles
DURING INITIAL CLIMB NR 2 ENGINE LOST TORQUE, THEN COMPLETELY LOST POWER. CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD. IN FLIGHT SHUT DOWN.